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A Performance Map For Ideal Air Breathing Pulse Detonation Engines
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Book Synopsis A Performance Map for Ideal Air Breathing Pulse Detonation Engines by : Daniel E. Paxson
Download or read book A Performance Map for Ideal Air Breathing Pulse Detonation Engines written by Daniel E. Paxson and published by . This book was released on 2001 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Performance Map for Ideal Air Breathing Pulse Detonation Engines ... Nasa by : United States. National Aeronautics and Space Administration
Download or read book A Performance Map for Ideal Air Breathing Pulse Detonation Engines ... Nasa written by United States. National Aeronautics and Space Administration and published by . This book was released on 2003* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721584437 Total Pages :32 pages Book Rating :4.5/5 (844 download)
Book Synopsis Optimal Area Profiles for Ideal Single Nozzle Air-Breathing Pulse Detonation Engines by : National Aeronautics and Space Administration (NASA)
Download or read book Optimal Area Profiles for Ideal Single Nozzle Air-Breathing Pulse Detonation Engines written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-20 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of cross-sectional area variation on idealized Pulse Detonation Engine performance are examined numerically. A quasi-one-dimensional, reacting, numerical code is used as the kernel of an algorithm that iteratively determines the correct sequencing of inlet air, inlet fuel, detonation initiation, and cycle time to achieve a limit cycle with specified fuel fraction, and volumetric purge fraction. The algorithm is exercised on a tube with a cross sectional area profile containing two degrees of freedom: overall exit-to-inlet area ratio, and the distance along the tube at which continuous transition from inlet to exit area begins. These two parameters are varied over three flight conditions (defined by inlet total temperature, inlet total pressure and ambient static pressure) and the performance is compared to a straight tube. It is shown that compared to straight tubes, increases of 20 to 35 percent in specific impulse and specific thrust are obtained with tubes of relatively modest area change. The iterative algorithm is described, and its limitations are noted and discussed. Optimized results are presented showing performance measurements, wave diagrams, and area profiles. Suggestions for future investigation are also discussed. Paxson, Daniel E. Glenn Research Center NASA/TM-2003-212496, AIAA Paper 2003-4512, NAS 1.15:212496, E-14057
Book Synopsis Optimal Area Profiles for Ideal Single Nozzle Air-Breathing Pulse Detonation Engines by : Daniel E. Paxson
Download or read book Optimal Area Profiles for Ideal Single Nozzle Air-Breathing Pulse Detonation Engines written by Daniel E. Paxson and published by . This book was released on 2003 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Model for the Performance of Air-breathing Pulse Detonation Engines by : E. Wintenberger
Download or read book A Model for the Performance of Air-breathing Pulse Detonation Engines written by E. Wintenberger and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Airbreathing Pulse Detonation Engine Performance by :
Download or read book Airbreathing Pulse Detonation Engine Performance written by and published by . This book was released on 2002 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Fundamentals of Idealized Air-breathing Pulse-detonation Engines by : J. A. C. Kentfield
Download or read book The Fundamentals of Idealized Air-breathing Pulse-detonation Engines written by J. A. C. Kentfield and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aircraft Propulsion and Gas Turbine Engines by : Ahmed F. El-Sayed
Download or read book Aircraft Propulsion and Gas Turbine Engines written by Ahmed F. El-Sayed and published by CRC Press. This book was released on 2017-07-06 with total page 1448 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft Propulsion and Gas Turbine Engines, Second Edition builds upon the success of the book’s first edition, with the addition of three major topic areas: Piston Engines with integrated propeller coverage; Pump Technologies; and Rocket Propulsion. The rocket propulsion section extends the text’s coverage so that both Aerospace and Aeronautical topics can be studied and compared. Numerous updates have been made to reflect the latest advances in turbine engines, fuels, and combustion. The text is now divided into three parts, the first two devoted to air breathing engines, and the third covering non-air breathing or rocket engines.
Book Synopsis Thrust Chamber Dynamics and Propulsive Performance of Airbreathing Pulse Detonation Engines by :
Download or read book Thrust Chamber Dynamics and Propulsive Performance of Airbreathing Pulse Detonation Engines written by and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermodynamic Efficiency of Air-breathing Pulse Detonation Engines by : Raja Kidambi
Download or read book Thermodynamic Efficiency of Air-breathing Pulse Detonation Engines written by Raja Kidambi and published by . This book was released on 1999 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Parametric Study of the Air-breathing Pulsed Detonation Engine by : S. Eidelman
Download or read book A Parametric Study of the Air-breathing Pulsed Detonation Engine written by S. Eidelman and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Thermodynamics of Air-breathing Pulse-detonation Engines by : J. A. C. Kentfield
Download or read book The Thermodynamics of Air-breathing Pulse-detonation Engines written by J. A. C. Kentfield and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 2003 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-3400 - 04-3449 by :
Download or read book 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-3400 - 04-3449 written by and published by . This book was released on 2004 with total page 570 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3900 - 02-3949 by :
Download or read book 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3900 - 02-3949 written by and published by . This book was released on 2002 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Direct-Connect Performance Evaluation of a Valveless Pulse Detonation Engine by : Nicole K. Wittmers
Download or read book Direct-Connect Performance Evaluation of a Valveless Pulse Detonation Engine written by Nicole K. Wittmers and published by . This book was released on 2004-12 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: Operational characteristics of a valveless pulse detonation engine system were characterized by experimental measurements of thrust, fuel flow, and internal gas dynamics. The multi-cycle detonation experiments were performed on an axis-symmetric engine geometry operating on an ethylene/air mixture. The detonation diffraction process from a small initiator combustor to a larger diameter main combustor in a continuous airflow configuration was evaluated during multi-cycle operation of a pulse detonation engine and was found to be very successful at initiating combustion of the secondary fuel/air mixture at high frequencies. The configuration was used to demonstrate the benefit of generating an overdriven detonation condition near the diffraction plane for enhanced transmission of the larger combustor. Results have shown that the addition of optical sensors, such as tunable diode lasers, to provide fuel profile data are invaluable for providing high fidelity performance results. The performance results demonstrated the ability of the valveless pulse detonation engine to run at efficiencies similar to valved pulse detonation engine geometries and may be a low-cost alternative to conventional air-breathing propulsion systems.
Book Synopsis 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-3350 - 04-3399 by :
Download or read book 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-3350 - 04-3399 written by and published by . This book was released on 2004 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt: